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GOE 652 AIRFOIL (goe652-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 652 AIRFOIL (goe652-il)
Reynolds number: 1,000,000
Max Cl/Cd: 135.65 at α=2.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe652-il-1000000.txt
Download as CSV file: xf-goe652-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 652 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.1024   0.06263   0.05951  -0.1711   0.8779   0.0524
 -12.250  -0.1192   0.05627   0.05293  -0.1778   0.8630   0.0529
 -12.000  -0.1239   0.05252   0.04905  -0.1811   0.8510   0.0532
 -11.750  -0.1242   0.04963   0.04606  -0.1833   0.8415   0.0535
 -11.500  -0.1242   0.04704   0.04338  -0.1849   0.8324   0.0538
 -11.250  -0.1222   0.04476   0.04100  -0.1862   0.8234   0.0540
 -11.000  -0.1191   0.04308   0.03931  -0.1865   0.8175   0.0544
 -10.750  -0.1127   0.04186   0.03807  -0.1862   0.8109   0.0548
 -10.500  -0.1092   0.04063   0.03680  -0.1856   0.8038   0.0553
 -10.250  -0.1023   0.03924   0.03540  -0.1860   0.7984   0.0556
 -10.000  -0.0929   0.03768   0.03383  -0.1870   0.7930   0.0559
  -9.750  -0.0832   0.03591   0.03202  -0.1887   0.7871   0.0563
  -9.500  -0.0700   0.03424   0.03029  -0.1906   0.7807   0.0568
  -9.250  -0.0538   0.03254   0.02856  -0.1931   0.7763   0.0573
  -9.000  -0.0356   0.03057   0.02656  -0.1965   0.7719   0.0578
  -8.750  -0.0132   0.02883   0.02476  -0.2000   0.7671   0.0583
  -8.500   0.0123   0.02697   0.02282  -0.2043   0.7622   0.0588
  -8.250   0.0423   0.02517   0.02092  -0.2093   0.7567   0.0592
  -8.000   0.0767   0.02345   0.01920  -0.2148   0.7535   0.0603
  -7.750   0.1168   0.02124   0.01695  -0.2224   0.7491   0.0614
  -7.500   0.1597   0.01917   0.01479  -0.2298   0.7437   0.0625
  -7.250   0.2032   0.01738   0.01288  -0.2366   0.7380   0.0637
  -7.000   0.2463   0.01587   0.01126  -0.2425   0.7331   0.0648
  -6.750   0.2986   0.01352   0.00882  -0.2516   0.7285   0.0669
  -6.500   0.3418   0.01204   0.00723  -0.2569   0.7230   0.0687
  -6.250   0.3771   0.01146   0.00654  -0.2590   0.7179   0.0702
  -6.000   0.4124   0.01093   0.00593  -0.2610   0.7127   0.0723
  -5.750   0.4468   0.01049   0.00548  -0.2626   0.7090   0.0748
  -5.500   0.4791   0.01025   0.00519  -0.2635   0.7040   0.0771
  -5.250   0.5122   0.00991   0.00481  -0.2646   0.6981   0.0805
  -5.000   0.5431   0.00978   0.00460  -0.2651   0.6912   0.0838
  -4.750   0.5756   0.00950   0.00433  -0.2660   0.6858   0.0881
  -4.500   0.6067   0.00936   0.00416  -0.2664   0.6800   0.0923
  -4.250   0.6377   0.00922   0.00399  -0.2668   0.6740   0.0971
  -4.000   0.6685   0.00912   0.00385  -0.2672   0.6686   0.1016
  -3.750   0.6994   0.00900   0.00373  -0.2676   0.6633   0.1061
  -3.500   0.7299   0.00892   0.00362  -0.2678   0.6569   0.1105
  -3.250   0.7594   0.00890   0.00354  -0.2679   0.6494   0.1149
  -3.000   0.7900   0.00882   0.00346  -0.2681   0.6438   0.1193
  -2.750   0.8200   0.00878   0.00340  -0.2682   0.6367   0.1241
  -2.500   0.8490   0.00880   0.00336  -0.2681   0.6287   0.1287
  -2.250   0.8791   0.00875   0.00332  -0.2683   0.6222   0.1338
  -2.000   0.9082   0.00877   0.00329  -0.2682   0.6140   0.1381
  -1.750   0.9372   0.00880   0.00329  -0.2681   0.6063   0.1433
  -1.500   0.9667   0.00882   0.00329  -0.2680   0.6001   0.1476
  -1.250   0.9958   0.00884   0.00330  -0.2680   0.5930   0.1531
  -1.000   1.0241   0.00892   0.00334  -0.2677   0.5858   0.1580
  -0.750   1.0534   0.00894   0.00335  -0.2677   0.5800   0.1624
  -0.500   1.0821   0.00900   0.00340  -0.2675   0.5730   0.1678
  -0.250   1.1096   0.00913   0.00348  -0.2671   0.5656   0.1725
   0.000   1.1388   0.00915   0.00350  -0.2670   0.5600   0.1775
   0.250   1.1670   0.00923   0.00358  -0.2667   0.5525   0.1820
   0.500   1.1941   0.00938   0.00366  -0.2663   0.5442   0.1857
   0.750   1.2223   0.00946   0.00373  -0.2660   0.5371   0.1883
   1.000   1.2499   0.00956   0.00379  -0.2657   0.5283   0.1937
   1.250   1.2774   0.00967   0.00389  -0.2653   0.5209   0.1977
   1.500   1.3050   0.00978   0.00398  -0.2649   0.5132   0.2013
   1.750   1.3309   0.00998   0.00411  -0.2642   0.5041   0.2037
   2.000   1.3589   0.01004   0.00417  -0.2640   0.4957   0.2086
   2.250   1.3843   0.01025   0.00433  -0.2632   0.4838   0.2128
   2.500   1.4108   0.01040   0.00445  -0.2627   0.4722   0.2165
   2.750   1.4356   0.01064   0.00462  -0.2618   0.4585   0.2196
   3.000   1.4594   0.01092   0.00480  -0.2608   0.4416   0.2225
   3.250   1.4823   0.01125   0.00503  -0.2597   0.4198   0.2280
   3.500   1.5031   0.01168   0.00534  -0.2583   0.3949   0.2321
   3.750   1.5238   0.01211   0.00566  -0.2567   0.3759   0.2358
   4.000   1.5447   0.01251   0.00596  -0.2553   0.3625   0.2388
   4.250   1.5673   0.01279   0.00621  -0.2541   0.3537   0.2433
   4.500   1.5881   0.01314   0.00652  -0.2526   0.3451   0.2488
   4.750   1.6102   0.01335   0.00675  -0.2513   0.3407   0.2536
   5.000   1.6297   0.01362   0.00701  -0.2495   0.3362   0.2574
   5.250   1.6480   0.01394   0.00730  -0.2476   0.3315   0.2609
   5.500   1.6655   0.01430   0.00766  -0.2455   0.3262   0.2678
   5.750   1.6869   0.01452   0.00793  -0.2442   0.3238   0.2736
   6.000   1.7075   0.01479   0.00821  -0.2427   0.3210   0.2783
   6.250   1.7266   0.01511   0.00854  -0.2410   0.3177   0.2836
   6.500   1.7450   0.01548   0.00893  -0.2392   0.3145   0.2907
   6.750   1.7621   0.01591   0.00937  -0.2372   0.3111   0.2969
   7.000   1.7777   0.01643   0.00987  -0.2350   0.3076   0.3012
   7.250   1.7974   0.01677   0.01026  -0.2336   0.3057   0.3084
   7.500   1.8177   0.01708   0.01064  -0.2322   0.3038   0.3152
   7.750   1.8368   0.01747   0.01105  -0.2307   0.3011   0.3210
   8.000   1.8547   0.01792   0.01153  -0.2290   0.2982   0.3268
   8.250   1.8710   0.01847   0.01210  -0.2271   0.2953   0.3339
   8.500   1.8862   0.01910   0.01274  -0.2252   0.2922   0.3399
   8.750   1.8987   0.01990   0.01354  -0.2229   0.2883   0.3444
   9.000   1.9182   0.02032   0.01402  -0.2216   0.2864   0.3509
   9.250   1.9372   0.02079   0.01455  -0.2203   0.2841   0.3577
   9.500   1.9541   0.02138   0.01518  -0.2187   0.2810   0.3639
   9.750   1.9700   0.02207   0.01587  -0.2171   0.2779   0.3692
  10.000   1.9834   0.02292   0.01675  -0.2152   0.2744   0.3758
  10.250   1.9949   0.02393   0.01777  -0.2132   0.2699   0.3816
  10.500   2.0131   0.02451   0.01841  -0.2119   0.2674   0.3873
  10.750   2.0293   0.02525   0.01919  -0.2105   0.2635   0.3943
  11.000   2.0431   0.02617   0.02013  -0.2088   0.2587   0.4015
  11.250   2.0522   0.02746   0.02142  -0.2068   0.2530   0.4074
  11.500   2.0680   0.02829   0.02229  -0.2054   0.2488   0.4145
  11.750   2.0795   0.02946   0.02348  -0.2037   0.2418   0.4222
  12.000   2.0878   0.03092   0.02492  -0.2018   0.2340   0.4293
  12.250   2.0955   0.03248   0.02648  -0.1999   0.2235   0.4380
  12.500   2.1002   0.03435   0.02831  -0.1978   0.2114   0.4466
  12.750   2.1008   0.03665   0.03058  -0.1956   0.1991   0.4552
  13.000   2.1021   0.03898   0.03288  -0.1935   0.1889   0.4661
  13.250   2.1053   0.04121   0.03512  -0.1917   0.1825   0.4789
  13.500   2.1079   0.04356   0.03749  -0.1900   0.1762   0.4949
  13.750   2.1148   0.04555   0.03956  -0.1887   0.1729   0.5218
  14.000   2.1214   0.04763   0.04172  -0.1874   0.1694   0.5716
  14.250   2.1248   0.04985   0.04436  -0.1861   0.1658   1.0000
  14.500   2.1295   0.05219   0.04671  -0.1848   0.1624   1.0000
  14.750   2.1371   0.05425   0.04882  -0.1838   0.1604   1.0000
  15.000   2.1439   0.05643   0.05104  -0.1827   0.1579   1.0000
  15.250   2.1476   0.05902   0.05366  -0.1816   0.1553   1.0000
  15.500   2.1493   0.06191   0.05658  -0.1806   0.1523   1.0000
  15.750   2.1504   0.06492   0.05962  -0.1796   0.1496   1.0000
  16.000   2.1595   0.06693   0.06170  -0.1789   0.1480   1.0000
  16.250   2.1670   0.06917   0.06398  -0.1782   0.1459   1.0000
  16.500   2.1697   0.07209   0.06695  -0.1775   0.1434   1.0000
  16.750   2.1715   0.07513   0.07002  -0.1768   0.1406   1.0000
  17.000   2.1681   0.07898   0.07391  -0.1763   0.1376   1.0000
  17.250   2.1765   0.08116   0.07615  -0.1758   0.1358   1.0000
  17.500   2.1810   0.08393   0.07898  -0.1754   0.1331   1.0000
  17.750   2.1816   0.08727   0.08235  -0.1750   0.1299   1.0000
  18.000   2.1775   0.09135   0.08646  -0.1748   0.1263   1.0000
  18.250   2.1816   0.09420   0.08937  -0.1746   0.1235   1.0000
  18.500   2.1818   0.09764   0.09285  -0.1745   0.1194   1.0000
  18.750   2.1755   0.10211   0.09734  -0.1747   0.1153   1.0000
  19.000   2.1753   0.10566   0.10093  -0.1748   0.1113   1.0000
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